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contributor authorT. Yoshida
contributor authorR. J. Goldstein
date accessioned2017-05-08T23:17:46Z
date available2017-05-08T23:17:46Z
date copyrightJuly, 1984
date issued1984
identifier issn1528-8919
identifier otherJETPEZ-26607#612_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98404
description abstractMeasurements are reported of the temperature and velocity fields above an adiabatic flat plate through which air is injected via a row of circular injection holes inclined at an angle of 35 deg to the surface. A mainstream flow of air over the plate is present, with Reynolds number based on stream velocity and injection tube diameter of 3.4 × 103 throughout the experiments. The boundary layer approaching the row of holes is either laminar or turbulent and either fully developed laminar or turbulent pipe flow is present in the injection hole (in the absence of the mainstream). The jets emanate from the holes at a mass flux rate from 0.2 to 2.0 times that of the mainstream flow. Key findings are: (i) a laminar jet can penetrate into the main flow with a smaller mass flux than a turbulent jet; and (ii) a turbulent-approaching boundary layer generates a wider domain of interaction between the jets and the mainstream than a laminar-approaching boundary layer for the same blowing rate.
publisherThe American Society of Mechanical Engineers (ASME)
titleOn the Nature of Jets Issuing From a Row of Holes Into a Low Reynolds Number Mainstream Flow
typeJournal Paper
journal volume106
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3239614
journal fristpage612
journal lastpage618
identifier eissn0742-4795
keywordsReynolds number
keywordsJets
keywordsFlow (Dynamics)
keywordsTurbulence
keywordsBoundary layers
keywordsPipe flow
keywordsFlat plates
keywordsTemperature AND Measurement
treeJournal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 003
contenttypeFulltext


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